US9523343B2  Powerconversion installation including a hydraulic machine provided with a runner  Google Patents
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 US9523343B2 US9523343B2 US14/113,206 US201214113206A US9523343B2 US 9523343 B2 US9523343 B2 US 9523343B2 US 201214113206 A US201214113206 A US 201214113206A US 9523343 B2 US9523343 B2 US 9523343B2
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 238000006243 chemical reaction Methods 0 claims description title 6
 230000002093 peripheral Effects 0 abstract claims description 46
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 230000002829 reduced Effects 0 description 8
 230000001808 coupling Effects 0 description 5
 238000010168 coupling process Methods 0 description 5
 238000005859 coupling reaction Methods 0 description 5
 230000001052 transient Effects 0 description 3
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 230000014509 gene expression Effects 0 description 2
 239000007787 solids Substances 0 description 2
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 F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
 F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
 F03B—MACHINES OR ENGINES FOR LIQUIDS
 F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
 F03B3/12—Blades; Bladecarrying rotors

 F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
 F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
 F03B—MACHINES OR ENGINES FOR LIQUIDS
 F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
 F03B3/02—Machines or engines of reaction type; Parts or details peculiar thereto with radial flow at highpressure side and axial flow at lowpressure side of rotors, e.g. Francis turbines

 F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
 F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
 F03B—MACHINES OR ENGINES FOR LIQUIDS
 F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
 F03B3/04—Machines or engines of reaction type; Parts or details peculiar thereto with substantially axial flow throughout rotors, e.g. propeller turbines
 F03B3/06—Machines or engines of reaction type; Parts or details peculiar thereto with substantially axial flow throughout rotors, e.g. propeller turbines with adjustable blades, e.g. Kaplan turbines

 F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
 F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
 F03B—MACHINES OR ENGINES FOR LIQUIDS
 F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
 F03B3/12—Blades; Bladecarrying rotors
 F03B3/121—Blades, their form or construction

 F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
 F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
 F03B—MACHINES OR ENGINES FOR LIQUIDS
 F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
 F03B3/12—Blades; Bladecarrying rotors
 F03B3/125—Rotors for radial flow at highpressure side and axial flow at lowpressure side, e.g. for Francistype turbines

 F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
 F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01F04
 F05B—INDEXING SCHEME RELATING TO MACHINES OR ENGINES OTHER THAN NONPOSITIVEDISPLACEMENT MACHINES OR ENGINES, TO WIND MOTORS, TO NONPOSITIVE DISPLACEMENT PUMPS, AND TO GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY
 F05B2240/00—Components
 F05B2240/20—Rotors
 F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor

 F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
 F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01F04
 F05B—INDEXING SCHEME RELATING TO MACHINES OR ENGINES OTHER THAN NONPOSITIVEDISPLACEMENT MACHINES OR ENGINES, TO WIND MOTORS, TO NONPOSITIVE DISPLACEMENT PUMPS, AND TO GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY
 F05B2250/00—Geometry
 F05B2250/70—Shape
 F05B2250/71—Shape curved
 F05B2250/712—Shape curved concave

 Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSSSECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSSREFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
 Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
 Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
 Y02E10/00—Energy generation through renewable energy sources
 Y02E10/20—Hydro energy
 Y02E10/22—Conventional, e.g. with dams, turbines and waterwheels
 Y02E10/223—Turbines or waterwheels, e.g. details of the rotor
Abstract
Description
This application is a U.S. National Phase of International Application No.: PCT/EP2012/057285, filed Apr. 20, 2012, designating the U.S., and published in French as WO 2012/143518 on Sep. 13, 2012, which claims the benefit of French Patent Application No. 1153428 filed Apr. 20, 2011.
This invention relates to a Francis runner for a hydraulic machine intended to be passed through by a forced flow of water. When the machine is a turbine, such a flow has for effect to drive the runner in rotation and when the machine is a pump, such a flow results from this rotation. Moreover, this invention relates to a hydraulic machine provided with such a runner. On the other hand, this invention relates to a powerconversion installation including such a hydraulic machine.
Conventionally, installation for converting hydraulic power into electrical power comprises a hydraulic machine which operates in turbine mode and which is passed through by a forced flow of water of which the rate is controlled by a distributor. The runner of the turbine drives in rotation a shaft connected to an alternator. In order to couple the alternator to the electrical network, the rotation speed of the turbine must be stable, in order for the frequency of the electrical signal at the output of the alternator to be equal to the frequency of the electrical network. The frequency of the electrical network is 50 Hz in Europe, but this value can be 60 Hz in other territories, for example in the United States. As long as the machine is not coupled to the network, the torque of the runner is zero. During transient operating phases, pressure fluctuations in the flow cause instabilities, in such a way that the rotation speed of the runner of the turbine is not stabilised and the alternator cannot be coupled to the electrical network. In particular, during the starting of the turbine, the distributor opens gradually, causing oscillations of the rotation speed of the runner of the turbine. Then, when the desired opening of the distributor is reached, the alternator is coupled to the electrical network as soon as the rotation speed of the runner is stable and reaches a synchronous speed.
The graph of
The small reduced rotation speeds of the turbine, on the left portion of the graph, correspond to large heads, while the large reduced rotation speeds of the turbine, on the right portion of the graph, correspond to small heads. The points P1 to P6 are located respectively at the intersection between the curves C1 to C6 and a horizontal straight line corresponding to a zero reduced torque. The points P1 to P6 therefore give a reduced rotation speed of the runner making it possible to couple the alternator to the electrical network. It is known that, in such a graph, the operating points for which the slope of the curve is negative correspond to a stable operation of the turbine, in other words at a stable rotation speed of the runner. Inversely, the operating points for which the slope of the curve is positive correspond to an unstable rotation speed of the runner, which does not make it possible to couple the alternator to the network. Conventionally, it is sought to be able to operate the turbine for the smallest heads possible, while still retaining a negative slope.
For the runner 100 of prior art, it is observed that for the point P1, which corresponds to a first opening of the distributor for a relatively substantial head, the slope of the curve C1 is negative and the rotation speed is stable. With regards to the point P3, which corresponds to smaller head for a second opening of the distributor, the curve C3 is approximately vertical which means that the rotation speed of the runner 100 of prior art is not very stable. Finally, the curve C5 is in the shape of an S and its slope at the point P5 is positive, which corresponds to an unstable rotation speed of the runner 100.
In conclusion, the runner 100 of prior art does not make it possible, alone, to stabilise its rotation speed for relatively small heads.
With the purpose of stabilising the rotation speed of a runner of prior art, it is known to use a turbine with an additional coupling device which consists in desynchronising wicket gates. These wicket gates are distributed around the runner and can be desynchronised, i.e. it is possible to orient them differently in relation to one another in order to vary around the runner the rate of the flow for the purposes of obtaining a curve with a negative slope in what is shown in
US2005/013691 discloses a Francis runner comprising a crown and a belt, between which extend vanes having an inwardly curved leading edge of which the convexity is circumferential. As such, the leading edges each comprise an intermediate point, located at the bottom of the curved shape of the leading edge. This runner has a geometry such that the radius of a first connection point between the leading edge and the crown is smaller than the radius of the intermediate point. This geometry does not make it possible to improve the stability of the rotation speed of the runner, during the coupling phases on the electrical network.
It is these disadvantages more particularly that the invention intends to overcome by proposing a turbine runner of which the specific geometry makes it possible to stabilise the rotation speed of the runner during transient starting phases, for relatively small heads.
To this effect, the invention has for purpose a Francis runner for a hydraulic machine, intended to be passed through by a forced flow of water, comprising:

 a wheel which is rotationally symmetrical about an axis of rotation of the runner,
 a crown which is rotationally symmetrical about the axis of rotation and facing the wheel,
 a plurality of inwardly curved vanes, integral with the wheel and with the crown and each having a central edge in the vicinity of the axis of rotation and a peripheral edge, opposite the central edge, which extends between the wheel and the crown and which is intended to firstly be passed through by the flow when the hydraulic machine is operating in turbine mode. In other words, when the hydraulic machine is operating in turbine mode, the flow runs from the peripheral edge towards the central edge.
The peripheral edge of at least one vane is curved, the concavity thereof facing toward the outside of the runner. A first distance, measured between any point on the peripheral edge and a straight line passing through, on the one hand, a first connection point between the peripheral edge and the wheel and, on the other hand, a second connection point between the peripheral edge and the crown is maximal on an intermediate point on the peripheral edge. The radius of the intermediate point is strictly smaller than the radius of the first connection point. The radius of the intermediate point is strictly smaller than the radius of the second connection point.
Due to the hollow shape of the peripheral edge of the vanes, which correspond to the leading edge when the hydraulic machine is operating in turbine mode, the turbine is made to operate for smaller heads, while still retaining a negative slope at the operating points making it possible to couple the alternator to the electrical network. This makes it possible to obtain a stable rotation speed and to rapidly couple the turbine to the electrical network without the need to add an additional coupling device, in particular, for small heads.
According to advantageous but not mandatory aspects of the invention, such a runner can incorporate one or several of the following characteristics, taken in any technically permissible combination:

 The intermediate point is the furthest from the straight line.
 The orthogonal projection of the intermediate point on the straight line is located in a zone which extends along the straight line and which is centred on the middle of the straight line. The height of the zone is less than 80% of a height of each vane, measured between the first connection point and the second connection point, more preferably less than 10%.
 The peripheral edge of the vanes is in the shape of a portion of circle, ellipse, parabola, or even any curve.
 A first ratio, having:
 as denominator, a height of a vane measured between the first connection point and the second connection point,
 as numerator, a maximum distance between the straight line and the peripheral edge,
 is between 0% and 200%, more preferably between 30% and 80%.
 The intermediate point of the peripheral edge is located midway between the connection points.
 In a first plane, parallel to the axis of rotation and perpendicular to a second plane which passes through an intersection between the crown and an average surface of the vane located between an external face and an internal face of the vane, and which extends this average surface, the external face is convex and the internal face is concave.
 In the first plane, the external face and the internal face are in the shape of a portion of circle, ellipse, parabola, and even any curve.
 A second ratio, having:
 as denominator, a height of the vane, measured between the first connection point and the second connection point,
 as numerator, a maximum distance, measured parallel to the first plane, between the straight line and the peripheral edge,
 is between 0% and 200%, more preferably between 10% and 40%.
 In the first plane, the intermediate point on the peripheral edge is located midway between the connection points.
 In the first plane, the peripheral edge is curved, with the concavity thereof facing in the same direction as the direction of rotation in turbine mode of the runner.
 A second distance, measured parallel to the first plane, between any point on the peripheral edge and the straight line, is maximal at the intermediate point.
The invention also has for purpose a hydraulic machine provided with such a runner.
Advantageously, when the machine is operating in turbine mode, the flow first hits the external face of the vanes.
Finally, the invention relates to powerconversion installation including such a hydraulic machine.
The invention shall be well understood other advantages of the latter shall appear when reading the following description of a runner provided on a hydraulic machine which belongs to a powerconversion installation, given solely by way of example and in reference to the annexed drawings wherein:
The installation I shown in
The runner R comprises, furthermore, nine vanes 21 integral with the wheel 1 and with the crown 12 and which extend between the wheel 1 and the crown 12 about the axis Z. In
An object here is qualified as “central” when it is located in the vicinity of the axis Z, in opposition to the adjective “peripheral” which designates an object which is separated from the axis Z.
Each vane 21 has an inwardly curved shape between a peripheral end 22 of the vane 21 and a central end 23 of the vane 21. This inwardly curved shape constitutes a main curvature of the vane 21 essentially in the shape of a portion of a spiral. Each vane 21 has a peripheral edge 212, located at the periphery of the wheel 1 and a central edge 211, facing toward the axis Z. Each vane 21 is delimited par an external face 213, outside of the main curvature of the vane 21, and par an internal face 214, inside the main curvature of the vane 21. The faces 213 and 214 join together on the central edge 211 and on the peripheral edge 212.
When the machine M is operating in turbine mode, the flow E first hits the external face 213 of the vanes 21. As can be seen in
When the hydraulic machine M is operating in turbine mode, the peripheral edge 212 of each vane 21 forms a leading edge and the central edge 211 forms a trailing edge. The leading edge is intended to be passed through firstly by the flow E when the hydraulic machine M is operating in turbine mode. In other words, in turbine mode, the fluid flows from the peripheral edge towards the central edge. The description given hereinafter for the turbine mode uses these expressions “leading edge” and “trailing edge”; it can be transposed to the case where the runner is operating in pump mode by inverting these expressions.
A denotes the connection point of the wheel 1 with the leading edge 212 of each vane 21. B denotes the connection point of the wheel 1 with the trailing edge 211 of each vane 21. Similarly, C denotes the connection point of the crown 12 with the leading edge 212 of each vane 21 and D denotes the connection point of the crown 12 with the trailing edge 211 of each vane 21.
Ra, Rb, Rc or Rd respectively denote the radius of the point A, B, C or D. Each radius Ra, Rb, Rc and Rd is the distance, measured radially, between the axis Z and the point A, B, C or D.
The radius Rd is smaller than the radius Rb. The radiuses Ra and Rc are equal and are strictly larger than the radiuses Rb and Rd. In particular, the radius Rc is strictly larger than the radius Rb, which allows the machine M to be able to operate in pump mode, with satisfactory performance. When the machine M is operating in turbine mode, the pressure of the flow E, on point C, is greater than on point B.
S denotes an average surface of each vane 21 passing between the external 213 and internal 214 faces of the vane 21, at an equal distance from these faces. On the peripheral end 22 of the vane 21, the average surface S coincides with the leading edge 212. The surface S is shown in
L denotes a straight line passing through the points A and C of the leading edge 212. The straight line L is parallel to the axis of rotation Z of the runner R. Pa denotes a plane which passes through the straight line L and which is located in the extension of the average surface S on its intersection with the crown 12. The plane Pa passes through the semitangent to the left T of the peripheral end S1 of the trace on the crown 12 of the average surface S.
The leading edge 212 is curved and does not have any discontinuity. In other terms, the leading edge 212 is hollowed in the direction of the trailing edge 211, and its shape does not have any breaks. As such, the concavity of the leading edge 212 is facing toward the outside of the vane 21 and of the runner R, in particular in the plane Pa or in a plane parallel to the faces 213 or 214, in the vicinity of the leading edge 212.
In the plane Pa, the curved shape, hollowed, of the leading edge 212 is defined by a portion of circle, as is shown in
The leading edge 212 is symmetrical in relation to a plane P8 perpendicular to the straight line L which passes through an intermediate point N on the leading edge 212. The point N is the point on the leading edge 212 the furthest from the straight line L.
D21 denotes a distance between the point N and the straight line L and H denotes a height of the leading edge 212, measured between the points A and C, along the straight line L. The distance D21 is the maximum distance between the leading edge 212 and the straight line L.
In the example shown, the distance D21 is measured perpendicularly to the straight line L. Let d1 be the distance between the straight line L and any point P on the leading edge 212, measured perpendicularly to the straight line L. Let G be the orthogonal projection of the point P on the straight line L. The distance d1 is measured between the points P and G. The distance d1 is the projection of the vector {right arrow over (PG)} in the plane Pb. The distance d1 is zero at the point A and increases between the points A and N. At the point N, the distance d1 is maximal and is equal to the distance D21. Between the points N and C, the distance d1 decreases. At the point C, the distance d1 is zero.
As such, along the leading edge 212 and between the points A and C, the distance d1, expressed as a function of a distance L1 between the point A and the point G, comprises a single maximum and does not comprise any point of inflection.
The derivative of the distance d1 in relation to the distance L1 is positive between the points A and N, cancels out at the point N and is negative between the points N and C. The second derivative of the distance d1 in relation to the distance L1 is negative between the points A and C.
A ratio having, as numerator, the distance D21 and, as denominator, the height H, is between 0% and 200%, more preferably between 30% and 80%.
F denotes a point of intersection between the straight line L and the plane P8. The distance between the point A and the point F is equal to the distance between the point F and the point C. In other words, the plane P8 is located midway between the points A and C, along the straight line L.
Rn denotes the radius of the point N, i.e. the distance, measured radially, between the axis Z and the point N. The distance Rn is strictly less than the distance Ra and than the distance Rc.
As can be seen in
More precisely, in the plane Pb, the external surface 213, the internal surface 214 and the average surface S, which coincides with the leading edge 212, are each defined by a portion of circle. C212 denotes the centre of the circle that defines the shape of the leading edge 212 and R212 its radius. Likewise, C213 and C214 denote the centre of the circles that define the shape of the external surface 213 and of the internal surface 214, and R213 and R214 their respective radius.
In light of this secondary curvature, the straight line which passes through the points F and N, along which is measured the distance D21, is inclined in relation to the plane Pa of
D22 denotes a distance measured parallel to the plane Pb between the point F and the point N. The distance D22 is the maximum distance, in a plane parallel to the plane Pb, between the straight line L and the leading edge 212. The distance D22 is the projection of the vector {right arrow over (FN)} in the plane Pb. In the same way, the distance D21 is the projection of the vector {right arrow over (FN)} in the plane Pa.
A second ratio having, as numerator, the distance D22 and, as denominator, the height H of the vane 21, is between 0% and 200%, more preferably between 10% and 40%.
Moreover, in the plane Pb, the external face 213 and the internal face 214 are symmetrical in relation to the plane P8. In other words, in the plane Pb, the point N on the leading edge 212 is located at midheight between the connection points A and C.
In the example shown, the distance D22 is measured perpendicularly to the straight line L. Let d2 be the distance between the straight line L and any point P on the leading edge 212 and the straight line L, measured parallel to the plane Pb and perpendicularly to the straight line L. The distance d2 is the projection of the vector {right arrow over (PG)} in the plane Pb. The distance d2 is measured between the points P and G, parallel to the plane Pb.
The distance d2 is zero at the point A and increases between the points A and N. At the point N, the distance d2 is maximal and is equal to the distance D22. Between the points N and C, the distance d2 decreases. At the point C, the distance d2 is zero. As such, along the leading edge 212 and between the points A and C, the distance d2, expressed as a function of the distance L1, comprises a single maximum and does not comprise any point of inflection. The derivative of the distance d2 in relation to the distance L1 is positive between the points A and N, cancels out at the point N and is negative between the points N and C. The second derivative of the distance d2 in relation to the distance L1 is negative between the points A and C.
The concavity of the secondary curvature of the vanes 21 is facing in the direction of rotation R1 of the runner R, when the machine M is operating in turbine mode. In other terms, in a section perpendicular to the trace of the average surface S on the crown 12, and in the view of
Rp, θp and Zp denote the cylindrical coordinates of any point P on each leading edge 212.
Rp is the radius of the point P. Let Pz be the orthogonal projection of the point P on the axis Z. The radius Rp is measured between the points Pz and P, according to a radial direction. At the point A, the radius Rp is equal to the radius Ra. The radius Rp decreases between the points A and N. At the point N, the radius Rp is minimal and is equal to the radius Rn. The radius Rp increases between the points N and C. At the point C, the radius Rp is equal to the radius Rc.
Zp is the height of the point P. Az denotes the orthogonal projection of the point A on the axis Z. The height Zp of the point P is the distance between the point Az and the point Zp.
Cz denotes the orthogonal projection of the point C on the axis Z. Along the leading edge 212 and between the points A and C, the radius Rp, expressed as a function of the height Zp, comprises a single minimum and does not comprise any point of inflection. The derivative of the radius Rp in relation to the height Zp is positive between the points A and N, cancels out at the point N and is negative between the points N and C. The second derivative of the radius Rp in relation to the distance Zp is positive between the points A and C.
θp is the angle of the point P, in cylindrical coordinates. The angle θp has a positive sign identical to the direction of rotation R1 of the runner R, when the machine M is operating in turbine mode. Let Da be a radial straight line passing through the point A and the axis Z. For each vane 21, a radial straight line D0 is considered, passing through the axis Z, such that a positive angle θ0, measured starting from the straight line D0 and to the straight line Da, is equal to 45°.
In the cylindrical coordinate system, the angle θp of the point P is defined starting from the straight line D0 and to a straight line Dp passing through the points Pz and P.
As can be seen in
As such, along the leading edge 212 and between the points A and C, the angle θp, expressed as a function of the height Zp, comprises a single minimum and does not comprise any point of inflection.
The derivative of the angle θp in relation to their height Zp is negative between the points A and N, cancels out at the point N and is positive between the points N and C. The second derivative of the angle θp in relation to the height Zp is positive between the points A and C.
During transient operating phases of the installation I, for example during the starting of the installation I, the alternator 5 is not coupled to the electrical network as the rotation speed of the runner R is not stable and does not allow the alternator 5 to deliver an electrical signal of which the frequency is equal to the frequency of the electrical network. For example, in Europe, the frequency of the electrical network is equal to 50 Hz. Thanks to the hollow shape of the leading edge 212 of the vanes 21, the flow E causes little, even no turbulence and instabilities, which allows the rotation speed of the runner R to be stabilised for the purposes of coupling the alternator 5 on the network.
The stability of the rotation speed of the runner R of the invention can be observed on the graph of
The shape curving towards the exterior of the veil of the vanes 21 makes it possible to accentuate the concavity of the leading edges 212 and to obtain a distance D21 that is relatively significant, without needing to hollow the leading edge 212 in an excessively pronounced manner, along the average surface S, in the direction of the trailing edge 211. This allows the hydraulic machine M, when it is operating in pump mode, to not excessively lose effectiveness.
No additional device is required in order to provide a satisfactory rotation speed, as the shape of the vanes 21 allows in itself the coupling of the alternator 5 on the network.
Alternatively, the straight line L is not parallel to the axis of rotation Z of the runner R. For example, the point C can be offset towards the trailing edge 211 in relation to the point A.
Alternatively, the concave shape of the leading edges 212 is defined by a portion of ellipse or of parabola, even by any curve.
In another alternative, the shape curved towards the exterior of the leading edge 212, of the external face 213 and of the internal face 214 of a vane 21 is defined by a portion of ellipse or of parabola, even by any curve.
Alternatively, only certain vanes 21 have their leading edge concave.
Alternatively, the point N is not exactly at midheight between the points A and C. The orthogonal projection of the intermediate point N on the straight line L is then located in a zone which extends, along the straight line L, starting from the middle F of the straight line L and on either side of the middle F by being centred on the middle. The height H2 of the zone is less than 80% of the height H of the vane 21, more preferably less than 10%.
Furthermore, the various alternatives and embodiments described hereinabove can be combined together, entirely or partially, in order to give rise to other implementations of the invention.
Claims (16)
Priority Applications (3)
Application Number  Priority Date  Filing Date  Title 

FR1153428A FR2974394A1 (en)  20110420  20110420  Wheel for hydraulic machine, hydraulic machine equipped with such wheel and energy conversion installation comprising such a hydraulic machine 
FR1153428  20110420  
PCT/EP2012/057285 WO2012143518A1 (en)  20110420  20120420  Runner for a hydraulic machine, hydraulic machine provided with such a runner, and powerconversion equipment including such a hydraulic machine 
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US20140050587A1 US20140050587A1 (en)  20140220 
US9523343B2 true US9523343B2 (en)  20161220 
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US14/113,206 Active 20331017 US9523343B2 (en)  20110420  20120420  Powerconversion installation including a hydraulic machine provided with a runner 
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US (1)  US9523343B2 (en) 
EP (1)  EP2699792B1 (en) 
KR (1)  KR101548145B1 (en) 
CN (1)  CN103649524B (en) 
CA (1)  CA2832987C (en) 
CL (1)  CL2013003029A1 (en) 
CO (1)  CO6801671A2 (en) 
ES (1)  ES2546853T3 (en) 
FR (1)  FR2974394A1 (en) 
PE (1)  PE20141180A1 (en) 
PT (1)  PT2699792E (en) 
RU (1)  RU2557837C2 (en) 
WO (1)  WO2012143518A1 (en) 
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CN104514252A (en) *  20140506  20150415  金纯信  Water turbine based power suction type closestool 
EP3276157A1 (en) *  20160725  20180131  GE Renewable Technologies  Hydraulic turbine 
GB2555374A (en) *  20160915  20180502  Paunovic Nenad  Impeller 
GB2565756A (en) *  20170710  20190227  Paunovic Nenad  Propulsion Device 
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WO1998005863A1 (en)  19960802  19980212  Kvaerner Energy A.S  Runner for francistype hydraulic turbine 
JPH10318117A (en)  19970520  19981202  Toshiba Corp  Impeller of fluid machine 
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KR20060061278A (en)  20041130  20060607  제너럴 일렉트릭 캐나다  Runner for francis type hydraulic turbine 
JP2007064018A (en)  20050829  20070315  Toshiba Corp  Francis type runner and hydraulic machine 
RU2321766C2 (en)  20060519  20080410  Открытое акционерное общество "Силовые машиныЗТЛ, ЛМЗ, Электросила, Энергомашэкспорт" (ОАО "Силовые машины")  Blade system for wheel of hydraulic turbine 
JP2010168903A (en) *  20090120  20100805  Hitachi Ltd  Centrifugal hydraulic machine 
KR20100120710A (en)  20080305  20101116  알스톰 하이드로 프랑스  Tipforming member for a wheel of a hydraulic machine, and wheel and hydraulic machine which are equipped with such a member 
CN102016295A (en)  20080422  20110413  耐欧立斯有限公司  Blade for a device for generating energy from a fluid flow 

2011
 20110420 FR FR1153428A patent/FR2974394A1/en not_active Withdrawn

2012
 20120420 ES ES12714732.0T patent/ES2546853T3/en active Active
 20120420 US US14/113,206 patent/US9523343B2/en active Active
 20120420 RU RU2013151262/06A patent/RU2557837C2/en active
 20120420 KR KR1020137029737A patent/KR101548145B1/en active IP Right Grant
 20120420 WO PCT/EP2012/057285 patent/WO2012143518A1/en active Application Filing
 20120420 PT PT127147320T patent/PT2699792E/en unknown
 20120420 EP EP12714732.0A patent/EP2699792B1/en active Active
 20120420 PE PE2013002364A patent/PE20141180A1/en active IP Right Grant
 20120420 CA CA2832987A patent/CA2832987C/en active Active
 20120420 CN CN201280019539.0A patent/CN103649524B/en active IP Right Grant

2013
 20131018 CL CL2013003029A patent/CL2013003029A1/en unknown
 20131018 CO CO13247919A patent/CO6801671A2/en active IP Right Grant
Patent Citations (15)
Publication number  Priority date  Publication date  Assignee  Title 

US147351A (en)  18740210  Improvement in waterwheels  
DE323190C (en)  19160109  19200717  Robert Dubs  Blade for Schnellaeuferwasserturbinen with sichelausschnittfoermigem meridian section 
US4479757A (en)  19820930  19841030  Dominion Engineering Works Limited  Blade configurations for Francistype turbine runners 
WO1998005863A1 (en)  19960802  19980212  Kvaerner Energy A.S  Runner for francistype hydraulic turbine 
JPH10318117A (en)  19970520  19981202  Toshiba Corp  Impeller of fluid machine 
DE10210426A1 (en)  20020309  20031023  Voith Siemens Hydro Power  Device for flow stabilization in hydraulic flow machines 
WO2004031573A1 (en)  20020926  20040415  Va Tech Hydro Gmbh & Co  Hydraulic machine rotor 
US20050013691A1 (en)  20030616  20050120  Kabushiki Kaisha Toshiba  Francis turbine 
CA2438429A1 (en)  20030822  20050222  General Electric Canada Inc.  Method of rebuilding francis turbine runners 
KR20060061278A (en)  20041130  20060607  제너럴 일렉트릭 캐나다  Runner for francis type hydraulic turbine 
JP2007064018A (en)  20050829  20070315  Toshiba Corp  Francis type runner and hydraulic machine 
RU2321766C2 (en)  20060519  20080410  Открытое акционерное общество "Силовые машиныЗТЛ, ЛМЗ, Электросила, Энергомашэкспорт" (ОАО "Силовые машины")  Blade system for wheel of hydraulic turbine 
KR20100120710A (en)  20080305  20101116  알스톰 하이드로 프랑스  Tipforming member for a wheel of a hydraulic machine, and wheel and hydraulic machine which are equipped with such a member 
CN102016295A (en)  20080422  20110413  耐欧立斯有限公司  Blade for a device for generating energy from a fluid flow 
JP2010168903A (en) *  20090120  20100805  Hitachi Ltd  Centrifugal hydraulic machine 
NonPatent Citations (4)
Title 

International Search Report re Application No. PCT/EP2012/057285, mailed on Aug. 1, 2012. 
Office Action (Decision of Patent Grant) issued on Aug. 1, 2015, by the Korean Patent Office in corresponding Korean Patent Application No. 1020137029737, and an English Translation of the Office Action. (3 pages). 
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Also Published As
Publication number  Publication date 

CA2832987C (en)  20150804 
CN103649524B (en)  20151125 
CL2013003029A1 (en)  20140530 
EP2699792B1 (en)  20150617 
FR2974394A1 (en)  20121026 
RU2013151262A (en)  20150527 
PE20141180A1 (en)  20140914 
CN103649524A (en)  20140319 
KR101548145B1 (en)  20150828 
ES2546853T3 (en)  20150929 
CO6801671A2 (en)  20131129 
WO2012143518A1 (en)  20121026 
EP2699792A1 (en)  20140226 
KR20140027248A (en)  20140306 
PT2699792E (en)  20151013 
US20140050587A1 (en)  20140220 
CA2832987A1 (en)  20121026 
RU2557837C2 (en)  20150727 
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